Garmin GTN 6 Series Instructions Manual
Garmin GTN 6 Series Instructions Manual

Garmin GTN 6 Series Instructions Manual

Eurocopter ec130 series
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Instructions for Continued Airworthiness
GTN 6XX/7XX - Eurocopter EC130 Series
as installed in
(Make and Model Aircraft)
Reg. No. ___________
S/N __________
Dwg. Number:
190-01007-K9 Rev. 1
Garmin International, Inc.
1200 E. 151st Street
Olathe, Kansas 66062 USA
Record of Revision
Rev.
Date
Description of Change
1
10/17/2013
Initial Release

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Summary of Contents for Garmin GTN 6 Series

  • Page 1 GTN 6XX/7XX - Eurocopter EC130 Series as installed in (Make and Model Aircraft) Reg. No. ___________ S/N __________ Dwg. Number: 190-01007-K9 Rev. 1 Garmin International, Inc. 1200 E. 151st Street Olathe, Kansas 66062 USA Record of Revision Rev. Date Description of Change...
  • Page 2 Company Proprietary Information This drawing and the specifications contained herein are the property of Garmin International or its subsidiaries and may not be reproduced or used in whole or in part as the basis for manufacture or sale of products without written permission.
  • Page 3: Table Of Contents

    Table of Contents INTRODUCTION ........................... 1 Purpose ............................1 Scope ............................1 Document Control ......................... 1 Permission to Use Certain Documents ..................1 Definitions ............................1 Terminology........................... 2 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ..............3 Introduction ............................ 3 Description of Alteration ........................ 3 Control, Operating, and Testing Information .................
  • Page 4: Introduction

    This document provides Instructions for Continued Airworthiness compliant with requirements of 14 CFR §27.1529, and Part 27 Appendix A. This ICA is to be used by the agency installing Garmin GTN 6XX/7XX navigators, GMA 35 audio panel, and additional equipment under the GTN 6XX/7XX Part 27 Approved Model List (AML) STC, and includes information required by the operator to adequately maintain installed items.
  • Page 5: Terminology

    1.6 Terminology Except where specifically noted, references made to the ‘GTN’ will equally apply to the GTN 625/635/650/725/750. Also, ‘GTN 7XX’ refers specifically to the GTN 725 and GTN 750, and ‘GTN 6XX’ refers specifically to the GTN 625, GTN 635, and GTN 650. Except where specifically noted, references made to the ‘EC 130 Series’...
  • Page 6: Instructions For Continued Airworthiness

    (MFD), NAV and COM transceiver, and GPS/WAAS navigator functions. The GTN 625/635/650 Navigators (Garmin Touch Navigation) are a family of 2.65-inch tall aviation panel mounted retro-fit products that are intended to supersede the Garmin 400W Series Navigators. The GTN 6XX product family consists of the GTN 625 GPS/WAAS navigator, the GTN 635 GPS/WAAS/COM navigator, and the GTN 650 GPS/WAAS/NAV/COM navigator.
  • Page 7: Control, Operating, And Testing Information

    The GMA 35 is mounted in a notch behind the GTN 7XX to free up mounting space in the flight deck instrument panel. Rotorcraft model specific installation of the GTN is documented in GTN 6XX/7XX PART 27 AML STC INSTALLATION MANUAL and Garmin 190-01007-H9 Rev. 1, “GTN 6XX/7XX Navigator Installation, Eurocopter EC 130B4/T2 Rotorcraft”.
  • Page 8 GPS signal acquisition time may be increased. There is no loss of function or accuracy of the GTN unit with a dead battery. The battery must be replaced by the Garmin factory repair station or factory authorized repair station. Test – Bonding Perform an electrical bonding check.
  • Page 9 Item Description/Procedure Interval Visual Inspection The GTN unit, GMA 35 (if installed), switches, and wiring To be performed harnesses should be inspected to ensure continued integrity of coincident with the installation in alignment with Eurocopter’s Standard the Eurocopter Practices Manual (MTC 20-07-02-[ ]). EC 130 600 flight hour inspection Conduct a visual check of the GTN unit, switches, GMA 35 (if...
  • Page 10: Table 2. Maintenance Intervals For Antennas Replaced Under This Stc

    Table 2. Maintenance Intervals for Antennas Replaced Under this STC Test – Bonding check An electrical bonding test must be performed on antennas Bond Check to GPS Antenna(s) installed by this STC. be performed (Only if antenna is 1. Gain access to the antenna installation. every 10 years or installed by this STC) 2.
  • Page 11: Troubleshooting Information

    Visual Inspection Visual inspection on the antenna To be performed (Only if antenna is 1. Clean the antenna with water and mild soap. coincident with installed by this STC) 2. Verify there are no cracks on the antenna and around the Eurocopter attachment fasteners.
  • Page 12 Figure 1 GTN STC Equipment Fuselage Station Location Instructions for Continued Airworthiness GTN 6XX/7XX - Eurocopter EC130 Series Page 9 of 21 190-01007-K9 Rev. 1...
  • Page 13: Table 3. Bill Of Materials

    Figure 2 depicts a typical installation performed in a Eurocopter EC 130T2. Figure 3 depicts a typical installation performed in a Eurocopter EC 130 B4. Figure 4 and Figure 5 show typical circuit breaker installation in EC 130 T2 and EC 130 B4. Table 3 provides the bill of materials in reference to Figure 2 and Figure 3.
  • Page 14 Figure 2. Typical GTN / GMA35 Installation in Eurocopter EC130T2 Instructions for Continued Airworthiness GTN 6XX/7XX - Eurocopter EC130 Series Page 11 of 21 190-01007-K9 Rev. 1...
  • Page 15 Figure 3. Typical GTN Installation in Eurocopter EC 130B4 Instructions for Continued Airworthiness GTN 6XX/7XX - Eurocopter EC130 Series Page 12 of 21 190-01007-K9 Rev. 1...
  • Page 16 Figure 4. Circuit Breaker Location in Typical GTN Installation Figure 5. Typical GTN Circuit Breaker Location in Eurocopter EC130B4 Instructions for Continued Airworthiness GTN 6XX/7XX - Eurocopter EC130 Series Page 13 of 21 190-01007-K9 Rev. 1...
  • Page 17 Figure 6. Typical Circuit Breaker Location in Eurocopter EC130T2 In the EC 130T2, for GTNs mounted in the pedestal, the circuit breaker panel is located on top of existing instrument panel support, as shown in Figure 6. In the EC 130T2, for GTNs mounted in the instrument Instructions for Continued Airworthiness GTN 6XX/7XX - Eurocopter EC130 Series Page 14 of 21 190-01007-K9 Rev.
  • Page 18: Table 4. Circuit Breaker Labels

    panel, the circuit breaker panel is located in the cargo area and tail boom, as shown in Figure 6. In the EC 130 B4, the circuit breakers for the GTN 6XX are located on top of instrument panel support, or the right hand side of the pedestal as shown in Figure 5.
  • Page 19 Figure 7. EC 130 Series Wire Harness and Coaxial Cable Routing Instructions for Continued Airworthiness GTN 6XX/7XX - Eurocopter EC130 Series Page 16 of 21 190-01007-K9 Rev. 1...
  • Page 20 2.7.2 Weight and Balance The weight and moment arm for each piece of equipment for the EC 130 B4 is depicted in Figure 8. The weight and moment arm for each piece of equipment for the EC 130 T2 is depicted in Figure 9. Figure 8.
  • Page 21: Diagrams

    Figure 9. EC 130 T2 Installation Weight and Balance Location 2.8 Diagrams Aircraft specific LRU locations and wire routing diagram forms are contained in Appendix A of this document. Completed forms are to be retained with the aircraft permanent records. Point-to-point wiring diagrams for the GTN, GMA 35, and interfaced equipment included with the aircraft permanent records.
  • Page 22: Data Relative To Structural Fasteners

    Flight Standards Inspectors or the certificate holder’s PMI have the required resources to respond to questions regarding this ICA. In addition, the customer may contact Garmin with questions regarding this equipment and its installation. Garmin Customer Support may be contacted during normal business hours via telephone 913-397-8200 or from the Garmin web site at www.flyGarmin.com.
  • Page 24: Appendix Aequipment Locations And Wire Routing

    APPENDIX A EQUIPMENT LOCATIONS AND WIRE ROUTING GTN 6XX/7XX STC Installation – Eurocopter EC 130 Series The following diagram must be completed to depict the location of all LRUs and antenna(s) along with the wire routing for the GTN 6XX/7XX and GMA 35 throughout the aircraft structure for the Eurocopter EC 130 rotorcraft.

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